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Li for a cylindrical shell REVIEWED
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Working note by Phil dated 3.26.05, installed in Appendix C of his transmission line notes. He finds the H field of a uniform current in a shell of inner radius a and thickness δ, integrates the magnetic energy (using Maple), and gets L. The a→0 limit gives the round wire value μ/8π, and the thin-shell limit gives (μ/6π)(δ/a). He compares this with a quoted flat-wire result and a published paper's different result, which he judges wrong. Some equations are garbled in the extraction.
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This is the Title PhL 3.26.05
This is now installed in Appendix C, and I found external verification for the result in a 1922 book!
A new problem:
Consider a cylindrical shell conductor of inner radius a and thickness δ. What is the DC internal inductance of such a shell?
First, compute the H field. The total area of the shell is this
A = π(a+δ)2 - πa2 = π [(a+δ)2 - a2]
If we assume a constant current density in this shell, we find that
Jz(r) = I/A =
The current enclosed by a loop of radius r is given by
Ienc(r) = ∫ dS Jz = 2π!Syntax Error, Irdr Jz(r)dS = 2π !Syntax Error, Ir' dr'
= 2π [r2-a2] (1/2) = I
The current enclosed at radii ranging from a to a+δ is this
Ienc(r) = I Ienc(r) = I
which I could have started off with, it is a completely obvious fact.
Now compute Hθ(r)
2πrH(r) = current enclosed = Ienc(r) = I dim OK
H(r) = (I/2πr)
u = (1/2)μ1 H2 = (1/2) μ1 ()2 (1/2π)2 I2
U = ∫dS u = 2π !Syntax Error, Idr r u = (1/2) μ1 ()2 (1/2π) I2 !Syntax Error, Idr r
Maple does the integral
which result we re-express in terms of the ratio b ≡ δ/a,
Given this expression for J, we have
U = (1/2) μ1 ()2 (1/2π) I2 J
= (1/2) μ1a-4 ()2 (1/2π) I2 J = (1/2) μ1a-4 () (1/2π) I2 J
and then
U = (1/2)L I2
so
L = μ1a-4 () (1/2π) J(b)
In the limit a→0 we have b→∞ and then J(b) = (b4a4)/4 so
L = μ1a-4 b-4 (1/2π) (b4a4)/4 = μ1 (1/8π)
which is the correct result for a solid round wire.
For a thin cylindrical shell, we instead take b→ 0. Maple tells us that
so that in this limit we get
Li = μ1a-4 (1/2π) { J(b) } = μ1a-4 (1/2π) (a4b/3) = μ1 (1/2π) (b/3) = (μ1/6π)b
= (μ1/6π)(δ/a) = (μ1/8π)(4/3)(δ/a)
Now if I crudely think of this as a rolled up microstrip of width w = 2πa then I am getting
Li = (μ1/8π) (4/3) (2πδ/w) = (μ1/8π) [8π/3] (δ/w)
This is not too different from the quoted result for an unrolled microstrip,
Li = (μi/8π) [(4π/3) a/b ] a/b << 1 (flat wire) // ≈ (μi/8π) [ 4.2 a/b ] (C.4.11)
I think my result is the right one!
It is true that the flat wire and the annulus have different H field distributions so that might account for the difference.
Amazingly I found as PDF which has these quotes
My result was μ1(1/4π)[ 3-4ln2] (δ/a), but their result is μ1(1/4π) (δ/a). They give this reference for their results
and I think I have access to that stuff now. I download the thing and save it. I then do OCR with Acrobat so I can search the thing. None of them come searchable for some reason. It is 48 pages long. But I don't see this formula in there. The result quoted does match my Appendix K high frequency result
Li(ω) = (1/ω) Im(Zs) = (1/ω) = μ1σ1δ2/2 = μ1 (1/4π) (δ1/a1)
except the quote shows some R' thing. I cannot find anything like this in that PDF! But I know exactly what they are saying. So no need for The BSTJ thing.
There is no H field inside my cylinder by the way. I think my result is correct and that airline PDF paper is a red herring result that is wrong.
So I will redo each step in the a = 0 limit and see where it disagrees with the round wire step.